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Beschleunigung
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Riptide C12-6

Nano V1 Rev 4 · firmware 1.65Secure logSecure logThe altimeter signed this log and it passed verification on upload, so the data is unchanged since the device wrote it.Signatures use Ed25519, which no current technology can forge.
Apogäum
229.6m
6.45 s after launch
Max. Aufstieg
98.57m/s
peak ascent
Max. während Brennen
37.68G
during the burn
Landung
30.72s
touchdown 8.33 m/s
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Flugzusammenfassung

The flight, moment by moment

Liftoff
0 s
Rampenwinkel9.4°
Abgangswinkel13.72°
Brennschluss (erster)
0.83 s
Höhe29.78 m
Geschwindigkeit87.170 m/s
Launch detected
0.838 s
Höhe30.01 m
Geschwindigkeit87.07 m/s
Möglicher Auswurf
6.072 s
Höhe226.11 m
Geschwindigkeit3.99 m/s
Apogäum
6.44 s
Höhe229.6 Meter
Max. Neigung bis Brennschluss13.55°
Landung
30.71 s
Höhe-0.13 m
Max. Abstieg-14.73 m/s

Stabilität25.2%Schlecht

Neigung bei Brennschluss (20%)76.3
20% · Rail angle 9.4°
Nick/Gier-Rate (30%)27.7
25% · Coning 161.1/267.3°/s
Coning · boost (25%)12.2
25% · Spin 539.5°/s
Schubgeradheit (15%)0
30% · Thrust 66.4%

Rocket information

Calculated from the flight data alone
Boost acceleration105.0 m/s²
average over the burn · 10.7 g
Coast deceleration15.5 m/s²
average · gravity plus drag
Ballistic coefficient169 kg/m²
fitted to the 5.61 s coast
Apogee lost to tilt2.12 m
flown vertical ≈ 231.7 m · from the tilt at burnout
Chute opening peak50.04 G
largest deceleration after ejection
Average descent rate9.18 m/s
ejection to landing · 24.64 s
Batterie & Temperatur 84% → 77% · Temperatur Start 34.47 → 33.34 °C · Start nach Einschalten 3m 27s

About the stability score

Worked out from the flight log between liftoff and 80% of apogee. It is independent of the angle the altimeter was mounted at, so it measures the flight rather than the fitting.

Neigung bei Brennschluss (20%)20%How close to vertical it left the rod.
Nick/Gier-Rate (30%)25%How much the nose swung off the rocket's own axis across the whole ascent.
Coning · boost (25%)25%The same swing during the burn, when it matters most.
Schubgeradheit (15%)30%How cleanly the motor pushed along the body.

Spin about the rocket's own axis is not counted against it — a fast, straight spin is stable. The figures beside the score are the raw measurements behind these four.

Höhe
Apogäum229.6 Meter
Zeit bis Apogäum6.44 s
Brennschluss-Höhe29.78 m
Max. Geschw.-Höhe-10.67 m
Auswurf-Höhe226.11 m
Lande-Höhe-0.13 m
Aufnahme-Höhe-114.68 m
Geschwindigkeit
Max. Aufstieg98.56 m/s
Max. Abstieg-14.73 m/s
Bei Brennschluss87.170 m/s
Abstiegsgeschw.-8.682 m/s
Auswurfgeschw.3.99 m/s
Landegeschw.-8.332 m/s
Beschleunigung
Max. während Brennen37.68 G
Max. Aufstieg37.68 G
Max. Abstieg50.04 G
Durchschn. Aufstieg1.28 G
Durchschn. Brennen10.9 G
Zeiten
Brennschluss (erster)0.83 s
Apogäum6.44 s
Möglicher Auswurf6.072 s
Landung30.71 s
Winkel
Rampenwinkel ?9.4° ± 0.35° unsicher, Halterung hat sich bewegt
Abgangswinkel ?13.7° unsicher, Halterung hat sich bewegt
Max. Neigung bis Brennschluss ?13.55°
Ausrichtung ?46.75°
Einbauversatz ?39.5°
Start-Roll42.00°
Start-Nick-22.82°
Max. Drehung (Brennen)2398.56 dps
Durchschn. Drehung (Brennen)444.29 dps
Staging
Stages detected1
Burnout (refined)0.838 s
Stage S1 burnout
flip0.829 s
drag0.951 s
sig0.980 s
Recovery
Single deploy
No dual deploy detected on this flight.
Allgemein
Upload-Datum20/09/26-11:43:03
Datenpunkte8720
Gesamte Aufnahmezeit48.136 s
Durchschn. Abtastrate/s181.1
Anzahl Sperren0
Start nach Einschalten3m 27s
ReferenzachseX
Batterie & Temperatur
Batterie Start84%
Batterie Ende77%
Temperatur Start34.47°C
Temperatur Ende33.34°C
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Benutzernotizen

Riptide on a Quest C12-6 at FOG 20/09/26

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Youtube-Video
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Flugbilder 0
Keine Bilder
Flown as
Rocket
None
not linked
Motor configuration
None
no motor recorded
Loaded weight
None
not entered
Flugmotoren
Keine Motoren zu diesem Flug hinzugefügt
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Verknüpfte Rakete
Keine Rakete mit diesem Flug verknüpft

Linked flights

Connect flights that belong together: a second altimeter flown in the same rocket, or the same rocket flown again. Linked flights appear on each other’s pages.

Apogee spread229.6 – 252 m
#2954 · Nano V1Same rocket · same day252 mView flight →

Startplatz, Datum & Uhrzeit

Klicken Sie auf die Karte, um Ihren Startplatz zu markieren. Wechseln Sie zwischen Karten- und Satellitenansicht.

Imagery © Esri, Maxar, Earthstar Geographics

Klicken Sie auf die Karte · Ziehen zum Anpassen

Canopy height from the Meta and WRI High Resolution Canopy Height Maps v2 (Meta and World Resources Institute, 2026; source imagery © 2016 Vantor), used under CC BY 4.0. Ground elevation built from Terrain Tiles (Mapzen and AWS Open Data), derived from 3DEP and GMTED courtesy of the U.S. Geological Survey, SRTM courtesy of NASA, and ETOPO1 courtesy of NOAA. Map and imagery credited on the view above.

No launch site has been set for this flight.

Flugdaten-Animation

FLIGHT 2950

229.6 Meters

ALTITUDE
0.00m
VELOCITY
0.00m/s
ACCEL
0.00G
TILT
0.00°
PITCH
0.00°
ROLL
0.00°
YAW
0.00°
TIME
0.00s
AWAITING LAUNCH
ALT
altimetercloud.com
LAUNCH T+0.00s LANDING

BURNOUT

Motor burn complete

Hinweis: Die Fluganimation erfordert eine feste Ausrichtung Ihres Höhenmessers. Kalibrieren Sie Ihre Sensoren für beste Ergebnisse.
Nano V1
Rocketry Ltd

Nano V1

Kompaktes Höhenmesser für kleine Raketen. Dieser Flug wurde mit einem geflogen: Nano V1.
Hardwareversion Rev 4Softwareversion 1.65Zuletzt online 20/09/26-11:43:03

Technische Daten

Elektronik

Mikrocontroller
ESP32-S232-bit ESP32-S2 240MHz
Beschleunigungssensor
ST LSM6DSO3232G 3-axis (SPI)
Barometer
Bosch BMP581300 to 1250 hPa within specification
Gyroskop
ST LSM6DSO322000 dgps 3-axis

Aufzeichnung

Maximale Abtastrate
833 Hz
Maximale Messwerte pro Aufzeichnung
38,000
Längste Aufzeichnung
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Elektronik

Mikrocontroller
ESP32-S232-bit ESP32-S2 240MHz
Beschleunigungssensor
ST LSM6DSO3232G 3-axis (I2C)
Barometer
Bosch BMP581300 to 1250 hPa within specification
Gyroskop
ST LSM6DSO322000 dgps 3-axis

Aufzeichnung

Maximale Abtastrate
833 Hz
Maximale Messwerte pro Aufzeichnung
38,000
Längste Aufzeichnung
1 h 3 minAt 10Hz although default settings are 433Hz with 1:8 hybrid mode

Größe, Gewicht und Akku

Größe
20 × 10 × 8.9 mm
Gewicht
1.65 g1.65 g mit dem kleinsten Akku
Akkuspannung
3 bis 4.2 V
Akkulaufzeit
5mit dem kleinsten Akku
Größe
20 × 10 × 8.9 mm
Gewicht
1.65 g1.65 g mit dem kleinsten Akku
Akkuspannung
3 bis 4.2 V
Akkulaufzeit
5mit dem kleinsten Akku

Dokumente

Flights from this altimeter

6 of 620 of 117

Settings, as they were for this flight

Allgemeine Flugeinstellungen
Prognosedruck
i
Set this to your local forecast pressure at sea level. This will offer you slightly improved accuracty for your flight, although it's not 100% essential every little helps!

Xcweather.co.uk is a decent place to grab pressures from for your location and time.
1013.2 mbar
Starterkennung
i
This is the altitude above the launch pad altitude where the altimeter will trigger itself into recording / flight mode.

The altimeter keeps a constant average of the pressure while waiting for launch, it uses a simple algorithm and the pre-flight buffers to do this. The most recent 120 samples (~4 seconds) are ignored so your pre-trigger altitude won't effect the ground baseline.

For almost all uses we suggest keeping this on the 25 Meter (~82 feet) default settings. If you want to test your altimeter by throwing it in the air, or are planning a very low flight you may want to lower the setting.
30 meters
Abtastverhältnis
i
The altimeter runs at 50Hz however you can record every sample or every X samples in order to extend the log time. For example if you set the ratio to 1 it will save 1:1 samples, or if you set it to 3 it will save 1 in 3 samples.
1:1:1 (400Hz)
Max. Abtastungen
i
This is the maximum samples the altimeter will log per flight. When it reaches this amount it will stop and save the recording.
38000
Aufnahme-Stopp
i
This setting is how the altimeter decides to stop recording. You can choose either 450 (~9s) or 900 (~18s) samples stable or it will record until the max samples limit unless you press the BUTTON in Manual stop mode.

The samples stable method waits for the devices altitude not to change for the set number of samples. This is defined by not changing by more than +/- 1.0 meters for 98% of the samples, it's a reliable method to stop the recording after landing within 8-10 seconds (300 sample) or 16-20 seconds (600 sample).
Auto: 8s stable altitude
Oversampling
i
Oversampling is a internal setting of the BMP 390 pressure sensor. It is how many samples are taken for each reading. By taking multiple samples for each pressure reading the altimeter reduces noise and increases the resolution of the output.

The sensor can run at 50 samples per second in 4X mode, so we suggest leaving it in this mode as it will offer the highest accuracy.
16x Oversampling
IIR-Filter
i
The IIR filter is another internal sensor for the BMP390 pressure sensor. It is a Infinite impulse response filter used to enhance pressure measurement accuracy by reducing noise. It's primarily for smoothing out rapid pressure changes.

We suggest not setting this too high as it will cause delay to changes in altitude if set very high.
COEFF 7
Druckfilter
i
This filter is a software Kalman filter that runs on the altimeters processor.

The Kalman filter uses a prediction step based on a system model and then a correction step using new measurements to refine its estimate, it creates accurate most certain results from data with noise in it.
TruePath
Sample speed
i
The sample rate of the altimeter's sensors. 50Hz takes 50 samples per second, 100Hz takes 100 samples per second for higher resolution data.
400 Hz
Hybrid mode
i
When enabled, the altimeter records at full speed during ascent then switches to half speed after apogee to extend recording time during descent.
Enabled
Sensorsynchronisation
i
The filters on the pressure sensor can cause it to lag very slightly behind the Accelerometer and Gyroscope data. The Sync sensors option detects how far out of sync these sensors are. It then corrects the Acceleration and Gyroscope readings to match the pressure sensor.
AKTIVIERT (46 samples / 114.88ms)
Ausrichtung
i
This is the orientation you intend to install the Altimeter in your rocket. It's needed to ensure completly accurate angles and orientation charts and reports. Check out the Manual for more information on this.
Down (text up)
IMU-Filter
i
The IMU filter, or fusion filter takes the data from each axis of the Gyroscope and Accelerometer to calculate the Pitch, Roll, Yaw and tilt angle from vertical. These filters can build up some discrepency over time so it's important to calibrate your sensors to minimise this.
Madgwick 6-Axis
Start-ALP
i
This is prevention against accidental launch detection.

With this disabled the launch is based only on pressure and something that creates a low pressure can trigger the flight by accident. For example pulling your nose cone off can even trigger it.

With this enabled the rocket also needs to have seen 8 samples (0.25 seconds) of acceleration above this setting in the last 3 seconds as well as the pressure drop to trigger. There is a backup trigger of 1.05 seconds of altitude being above the launch detect setting too.

There are very few situations where this option would cause issues, so we suggest leaving it on.
2.0G
Startsperre
i
When enabled, the altimeter locks out recording for a set period after power on to prevent false triggering during setup.
DISABLED
Statische Temperatur
i
A fixed temperature value used for altitude calculation when the external temperature sensor is disabled or not connected.
15 °C
Sensorkalibrierung
Kalibrierungsversätze für diesen Flug.
Gyroskop
X-0.793°
Y0.368°
Z0.201°
Beschleunigungssensor
X7.370 mG
Y-16.080 mG
Z-6.300 mG

Files

Where the altimeter signs its log, the file carries that signature and a tick beside it. A tick means the data is unchanged since the device wrote it, which is what a record claim needs.
CSV
2950.csv ✓ SIGNED
The log as columns of text. Opens in a spreadsheet, and in every simulator that reads flight data.
835 KB
LOG
2950.aclz ✓ SIGNED
The altimeter's own compressed log, exactly as the device wrote it. This is the file to keep for a record claim.
105 KB
Adjusted CSV2904 recalculated in your browser
The log recomputed for your own sea-level pressure and temperature. Columns: time, altitude as recorded and adjusted, raw altitude as recorded and adjusted, pressure.

This file is built here from the signed log, so it carries no signature of its own. Anyone verifying a claim should be sent to the flight page and build their own from the original.

Custom CSVbuilt in your browser
Pick any of the chart’s data sets, the worked-out ones included, and the part of the flight to cover. Values come in the units the chart is set to.
In the file
Time span

One row for every time any chosen data set has a sample. A data set with no sample at that time is left blank rather than filled in. Built from the chart’s data, so it carries no signature.

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